• Title/Summary/Keyword: 병진운동

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The Effect of Spanwise Flow and Wing Rotation on the Aerodynamic Characteristics in Flapping Motion (날개 길이방향 유동과 날개 회전이 날개짓 운동의 공기역학적 특성에 미치는 효과)

  • Oh, Hyun-Taek;Choi, Hang-Cheol;Chung, Jin-Taek;Kim, Kwang-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.9
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    • pp.753-760
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    • 2007
  • In a 3-D flapping motion, the spanwise flow is generated while the wing is moved on the stroke plane. And at the end of each stroke, the rotational circulation is generated due to a wing rotation. In this study, to evaluate the effect of spanwise flow and wing rotation on the aerodynamic characteristics in 3-D flap 753ping motion, a 3-D flapping motion was compared with a 2-D translating motion. In each flapping motion, the aerodynamic forces were measured with respect to the angles of attack and Reynolds number. The aerodynamic forces generated by 2-D translating motion were higher than those generated by 3-D flapping motion. While the lift of 3-D flapping motion was increased until the angle of attack $60^{\circ}$ at mid-stroke, the lift generated by 2-D translating motion was decreased above the angle of attack 40° at mid stroke. Also, at the end of each stroke, the aerodynamic forces were increased rapidly due to wing rotation.

One-link 탄성 ARM 선단의 위치제어 -병진 운동의 경우-

  • 유기호;이성철
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 1990.04a
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    • pp.46-52
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    • 1990
  • 위치결정 정도의 향상과 robot arm의 경량화및 운동의 고속화의 요구에따라 비교적 가벼운 중량에 비해 상대적으로 큰 하중을 다룰수 있으며 고속 동작도 가능한 우연성있는 robot arm의 동장이 필요하게 되었다. 본 연구에서는 ballscrew system으로 구성되어 병진운동을 하는 탄성 arm 선단의 위치를 제어하는 이론적인 해석을 하고, 실제의 실험장치를 통하여 선단의 위치를 제어 하므로써 system의 제어특성을 찾고자 한다.

An Analysis of Inelastic Neutron Scattering by Liquid Methane

  • Chung, Chang-Hyun;Shin, Won-Kee;Kim, Jin-Soo
    • Nuclear Engineering and Technology
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    • v.5 no.4
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    • pp.265-278
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    • 1973
  • The incoherent neutron scattering cross section of molecular liquids is analyzed using a damping function model for correlation functions of molecular translations and rotations. The present approach is different from recent works in that the scattering function is evaluated directly, not through the intermediate scattering function. The damping fuction is determined from a simple relation between its long-wavelength limit and the generalized frequency distribution function, and translation-rotation couplings are assumed to be neglected. A physical model is used for the translational motions of center-of-mass of a molecule, including properly its short-time and long-time behaviors. A simple model for the rotational motions is suggested which relates the damping function to the Fourier transform of the dipole correlation function, or equivalently, the infrared vibrational absorption spectrum. Theoretical absolute scattering intensities are computed for liquid methane and shown to be in satisfactory agreement with both thermal and cold neutron measurements.

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Development of Two Types of Novel Planar Translational Parallel Manipulators by Using Parallelogram Mechanism (평행사변형 기구를 이용한 평면 병렬형 병진운동 기구 개발)

  • Kim, Han-Sung
    • Journal of the Korean Society for Precision Engineering
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    • v.24 no.8 s.197
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    • pp.50-57
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    • 2007
  • In this paper, two types of novel planar Translational Parallel Manipulators (TPMs) by using parallelogram mechanism are conceived. One is made up of two Pa-P (Parallelogram-Prismatic) legs connecting the base to the moving platform. The other consists of two P-Pa legs, which is the kinematic inversion of the former. Since connecting links in a parallelogram mechanism are subject to only tensile/compressive load and all the heavy actuators are mounted at the base, the proposed manipulators can be applied for planar positioning/assembly tasks requiring high stiffness and high speed. The position, velocity, and statics are analyzed, and the design methodology using prescribed workspace and velocity transmission capability is presented. Finally, two types of prototype manipulators have been developed.

Design of the Vision Based Head Tracker Using Area of Artificial Mark (인공표식의 면적을 이용하는 영상 기반 헤드 트랙커 설계)

  • 김종훈;이대우;조겸래
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.34 no.7
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    • pp.63-70
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    • 2006
  • This paper describes research of using area of artificial mark on vision based head tracker system. A head tracker system consists of the translational and rotational motions which are detected by web camera. Results of the motion are taken from image processing and neural network. Because of the characteristics of cockpit, the specific color on the helmet is tracked for translational motion. And rotational motion is tracked via neural network. Ratio of two different colored area on the helmet is used as input of network. Neural network algorithms used, such as back-propagation and RBFN (Radial Basis Function Network). Both back-propagation using a characteristic of feedback and RBFN using a characteristic of statistics have a good performances for the tracking of nonlinear system such as a head motion. Finally, this paper analyzes and compares with tracking performance.

A Study on Translational and Rotational Velocity Performance Indices of Six-Degree-of-Freedom parallel Mechanism (6자유도를 갖는 병렬형 기구의 병진속도와 회전속도 성능 지표에 관한 연구)

  • Kim, Chan-Soo
    • Journal of Korea Game Society
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    • v.10 no.6
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    • pp.57-65
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    • 2010
  • In this paper, mobility performance indices are proposed which may be used to estimate characteristics of output velocity space in six-degree-of-freedom parallel mechanism. In order for manipulability and condition number to not suffer from lack of the physical meaning due to dimensional inhomogeneity, output space is partitioned into translational velocity space and rotational velocity space, respectively. In each space, mobility ellipsoids corresponding to unit input space are defined and two types of mobility performance in translational velocity spaces indices are derived. Two types of mobility performance in rotational velocity spaces indices are derived.

SDINS Simulator Based On Dual Quatemions (Dual Quaternion 기반 관성항법 시뮬레이터)

  • Sim, Ju-Yeong;Lee, Hyeong-Geun;Lee, Han-Seong;Park, Chan-Guk;Yu, Myeong-Jong
    • 한국항공운항학회:학술대회논문집
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    • 2005.11a
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    • pp.132-135
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    • 2005
  • 이체 쿼터니언(dual quaternion)은 선형 미분방정식으로 계산하는 쿼터니언을 회전운동과 병진운동을 동시에 취급하는 이체수(dual numbers)체계로 표현한 형태이다. 성능향상을 위해 이체 쿼터니언을 관성항법 알고리즘에 적용시킨 논문이 새로이 소개되었다. 기존 알고리즘과 새로운 알고리즘을 MATLAB으로 시뮬레이터를 작성하였으며, 정확도와 실행 속도 측면에서 성능을 평가하고자 한다.

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